Triple Seven ROOK 777 XC SUPERSTAR, User Manual

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Certification specimens
Class:
B
In accordance with EN standards 926-2:2005 & 926-1:2006:
PG_0547.2012
Date of issue (DMY):
09. 03. 2012
Manufacturer:
777 jadralna padala d.o.o.
Model:
Rook M
Serial number:
Configuration during flight tests
Paraglider Accessories
Maximum weight in flight (kg) 105 Range of speed system (cm) 20
Minimum weight in flight (kg) 80 Speed range using brakes (km/h) 14
Glider's weight (kg) 4.8 Range of trimmers (cm) 0
Number of risers 3 Total speed range with accessories (km/h) 28
Projected area (m2) 22.4
Harness used for testing (max weight) Inspections (whichever happens first)
Harness type ABS every 12 months or every 100 flying hours
Harness brand Sup' Air Warning! Before use refer to user's manual
Harness model Access Person or company having presented the
glider for testing: Aliaz Valic
Harness to risers distance (cm) 49
Distance between risers (cm) 46
1
A
2
A
3
A
4
A
5
A
6
A
7
A
8
A
9
B
10
B
11
A
12
A
13
B
14
B
15
A
16
A
17
A
18
A
19
A
20
B
21
A
22
A
23
A
24
0
Flight test report: PG_0547.2012 / page 2 of 3
Dive forward angle on exit / Change of course Dive forward 0° to 30° / Keeping
course
AD ive forward 0° to 30° / Entering a
turn of less than 90°
A
Cascade occursN oA No A
11. Exiting deep stall (parachutal stall) A
Deep stall achieved YesA YesA
RecoveryS pontaneous in less than 3 s AS pontaneous in less than 3 s A
Dive forward angle on exitD ive forward 0° to 30° AD ive forward 0° to 30° A
Change of course Changing course less than 45° AC hanging course less than 45° A
Cascade occursN oA No A
12. High angle of attack recoveryA
RecoveryS pontaneous in less than 3 s AS pontaneous in less than 3 s A
Cascade occursN oA No A
13. Recovery from a developed full stall B
Dive forward angle on exitD ive forward 0° to 30° AD ive forward 30° to 60° B
Collapse No collapse AN o collapse A
Cascade occurs (other than collapses) No AN oA
Rocking back Less than 45° A Less than 45° A
Line tension Most lines tight AM ost lines tight A
14. Asymmetric collapse B
With 50% collapse
Change of course until re-inflation / Maximum dive forward or
roll angle
Less than 90° / Dive or roll angle
15° to 45°
A Less than 90° / Dive or roll angle 0°
to 15°
A
Re-inflation behaviour Spontaneous re-inflation AS pontaneous re-inflation A
Total change of course Less than 360° A Less than 360° A
Collapse on the opposite side occursN oA No A
Twist occursN oA No A
Cascade occursN oA No A
With 75% collapse
Change of course until re-inflation / Maximum dive forward or
roll angle
90° to 180° / Dive or roll angle
15° to 45°
B 90° to 180° / Dive or roll angle 15°
to 45°
B
Re-inflation behaviour Spontaneous re-inflation AS pontaneous re-inflation A
Total change of course Less than 360° A Less than 360° A
Collapse on the opposite side occursN oA No A
Twist occursN oA No A
Cascade occursN oA No A
With 50% collapse and accelerator
Change of course until re-inflation / Maximum dive forward or
roll angle
Less than 90° / Dive or roll angle
15° to 45°
A Less than 90° / Dive or roll angle
15° to 45°
A
Re-inflation behaviour Spontaneous re-inflation AS pontaneous re-inflation A
Total change of course Less than 360° A Less than 360° A
Collapse on the opposite side occursN oA No A
Twist occursN oA No A
Cascade occursN oA No A
With 75% collapse and accelerator
Change of course until re-inflation / Maximum dive forward or
roll angle
90° to 180° / Dive or roll angle
15° to 45°
B 90° to 180° / Dive or roll angle 15°
to 45°
B
Re-inflation behaviour Spontaneous re-inflation AS pontaneous re-inflation A
Total change of course Less than 360° A Less than 360° A
Collapse on the opposite side occursN oA No A
Twist occursN oA No A
Cascade occursN oA No A
15. Directional control with a maintained asymmetric
collapse
A
Able to keep course YesA YesA
180° turn away from the collapsed side possible in 10 sY es AY es A
Amount of control range between turn and stall or spin More than 50 % of the
symmetric control travel
AM ore than 50 % of the symmetric
control travel
A
Flight test report: PG_0547.2012 / page 3 of 3
16. Trim speed spin tendency A
Spin occursN oA NoA
17. Low speed spin tendency A
Spin occursN oA NoA
18. Recovery from a developed spinA
Spin rotation angle after release Stops spinning in less than 90° AS tops spinning in less than 90° A
Cascade occursN oA NoA
19. B-line stallA
Change of course before release Changing course less than 45° AC hanging course less than 45° A
Behaviour before release Remains stable with straight
span
AR emains stable with straight span A
RecoveryS pontaneous in less than 3 sA Spontaneous in less than 3 sA
Dive forward angle on exitD ive forward 0° to 30° AD ive forward 30° to 60° A
Cascade occursN oA NoA
20. Big earsB
Entry procedureD edicated controls AS tandard technique A
Behaviour during big earsS table flight AS table flight A
RecoveryS pontaneous in 3 s to 5 s BS pontaneous in less than 3 sA
Dive forward angle on exitD ive forward 0° to 30° AD ive forward 0° to 30° A
21. Big ears in accelerated flight A
Entry procedureD edicated controls AS tandard technique A
Behaviour during big earsS table flight AS table flight A
RecoveryS pontaneous in 3 s to 5 s AS pontaneous in less than 3 sA
Dive forward angle on exitD ive forward 0° to 30° AD ive forward 0° to 30° A
Behaviour immediately after releasing the accelerator while
maintaining big ears
Stable flight AS table flight A
22. Behaviour exiting a steep spiralA
Tendency to return to straight flight Spontaneous exitA Spontaneous exitA
Turn angle to recover normal flight Less than 720°, spontaneous
recovery
A Less than 720°, spontaneous
recovery
A
Sink rate when evaluating spiral stability [m/s]1 61 8
23. Alternative means of directional controlA
180° turn achievable in 20 sY es AY es A
Stall or spin occursN oA NoA
24. Any other flight procedure and/or configuration
described in the user's manual
0
Procedure works as described not available0 not available0
Procedure suitable for novice pilots not available0 not available0
Cascade occurs not available0 not available0
25. Comments of test pilot
Comments
Flight test report: EN
Manufacturer 777 jadralna padala d.o.o. Certification number PG_0547.2012
Address Ulica Ane Ziherlove 10
1000 Ljubljana
Slovenia
Date of flight test 28. 02. 2012
RepresentativeA liaz Valic Place of test Villeneuve
Glider model Rook MC lassificationB
Trimmern o
Test pilot Thurnheer Claude Berruex Gilles
Harness Sup' Air - Altiplume M Sup' Air - Access
Total weight in flight (kg) 80 105
Flight test report: PG_0547.2012 / page 1 of 3
1. Inflation/Take-offA
Rising behaviour Smooth, easy and constant rising AS mooth, easy and constant rising A
Special take off technique requiredN oA No A
2. Landing A
Special landing technique requiredN oA No A
3. Speed in straight flight A
Trim speed more than 30 km/h YesA YesA
Speed range using the controls larger than 10 km/h YesA YesA
Minimum speed Less than 25 km/h A Less than 25 km/h A
4. Control movement A
Max. weight in flight up to 80 kg
Symmetric control pressure / travel not available0 not available0
Max. weight in flight 80 kg to 100 kg
Symmetric control pressure / travel Increasing / greater than 60 cm A not available0
Max. weight in flight greater than 100 kg
Symmetric control pressure / travel not available0 Increasing / greater than 65 cm A
5. Pitch stability exiting accelerated flight A
Dive forward angle on exitD ive forward less than 30° AD ive forward less than 30° A
Collapse occursN oA No A
6. Pitch stability operating controls during accelerated
flight
A
Collapse occursN oA No A
7. Roll stability and damping A
Oscillations Reducing AR educing A
8. Stability in gentle spirals A
Tendency to return to straight flightS pontaneous exitA Spontaneous exitA
9. Behaviour in a steeply banked turn B
Sink rate after two turns 12 m/s to 14 m/sA More than 14 m/sB
10. Symmetric front collapse B
Entry Rocking back less than 45° AR ocking back less than 45° A
RecoveryS pontaneous in 3 s to 5 s BS pontaneous in less than 3 sA
Dive forward angle on exit / Change of course Dive forward 0° to 30° / Keeping
course
AD ive forward 0° to 30° / Entering a
turn of less than 90°
A
Cascade occursN oA No A
With accelerator
Entry Rocking back less than 45° AR ocking back less than 45° A
RecoveryS pontaneous in 3 s to 5 s BS pontaneous in less than 3 sA